Every requirement, what satisfies and verifies it, and whether the spacecraft meets it.
SC-1 — The bus dry mass shall not exceed 1200 kg.
SC-2 — The high-gain antenna shall provide at least 40 dBi.
SC-3 — The radiator shall provide at least 2 m² of rejection area.
SC-4 — The spacecraft shall be passivated at end of mission.
Requirements with their satisfiers and verifiers
| shortName | name | satisfiedBy | verifiedBy | verifications |
|---|---|---|---|---|
| SC-1 | massLimit | Traceability::spacecraft::bus | Traceability::massMeasurement | 1 |
| SC-2 | downlinkGain | Traceability::spacecraft::antenna | Traceability::gainTest, Traceability::gainAnalysis | 2 |
| SC-3 | heatRejection | Traceability::spacecraft::radiator | 0 | |
| SC-4 | passivation | 0 |
Checks of the spacecraft against its requirements
| kind | name | path | verdict | condition |
|---|---|---|---|---|
| satisfaction | Traceability::spacecraft.bus | holds | ||
| verification | massMeasurement | Traceability::spacecraft.bus | holds | |
| satisfaction | Traceability::spacecraft.antenna | holds | ||
| verification | gainTest | Traceability::spacecraft.antenna | holds | |
| verification | gainAnalysis | Traceability::spacecraft.antenna | holds | |
| satisfaction | Traceability::spacecraft.radiator | violated | radiator.area >= 2.0 |